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A two-objective design optimisation approach for blending repairs of damaged compressor blisks

机译:一种双目标设计优化方法,用于混合损坏压缩机假围的修复

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The blending of compressor blades leads to a permanent modification of the blade geometry. According to these geometric changes, the modal properties of refurbished blades will generally differ from the nominal blade design. Currently, the structural integrity of refurbished blades is maintained by only allowing blends within predefined geometric limits, where the final geometry of the blend is based on a case-by-case decision made by the technician.This work contributes to repair decisions by utilising multi-objective optimisation methods to find structurally optimised blend designs. A parameterised blending model is introduced to uniquely specify the repair design for any blade geometry. Blend designs are analysed systematically by linking the blending model with the Finite Element model of a bladed sector. The influence of the blending shape is evaluated by means of blade-alone frequencies and vibration mode shapes. A two-objective optimisation problem is derived from the frequency tuning of blended blades. The first objective results from the deviation of natural frequencies from the nominal ones, the second objective considers the proximity of natural frequencies to resonance frequencies. Moreover, the approach is applied to one bladed sector of a compressor blisk. The sensitivities of the blend geometry regarding the first six vibration modes are studied. Two damage patterns at different positions at the leading edge of the blade are chosen to exemplarily demonstrate the capability of the proposed approach. For both damage patterns, the set of Pareto optimal solutions is found using Global Pattern Search. The courses of the Pareto frontiers clearly differ and are identified to be specific for each damage pattern. Depending on the damage pattern, discontinuous as well as continuous Pareto frontiers are determined. Providing Pareto optimal solutions for repair designs, the developed approach can be understood as a valuable complement to purely experience-based design decisions. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:压缩机叶片的混合导致叶片几何形状的永久性修改。根据这些几何变化,翻新刀片的模态性能通常与标称叶片设计不同。目前,通过允许在预定的几何限制内的混合中的混合来维持翻新刀片的结构完整性,其中混合的最终几何形状基于技术人员的逐个案例决策。本工作有助于通过利用多种来修复决策。 - 选择性优化方法,用于找到结构上优化的混合设计。引入参数化混合模型以唯一指定任何刀片几何的修复设计。通过将混合模型与Bladed Sector的有限元模型连接,系统地分析混合设计。通过刀片单独的频率和振动模式形状评估混合形状的影响。两个客观优化问题来自混合刀片的频率调谐。第一个目标是来自标称值的自然频率的偏差,第二个目标考虑了自然频率与共振频率的偏差。此外,该方法应用于压缩机闪烁的一个叶片扇区。研究了关于前六种振动模式的混合几何体的敏感性。选择在刀片前缘的不同位置处的两个损伤图案以示例性地证明了所提出的方法的能力。对于这两种伤害模式,使用全局模式搜索找到该组Pareto最佳解决方案。帕累托前沿的课程显然有所不同,并且被确定为特定于每个伤害模式。根据损坏模式,确定不连续的和连续的帕累托前沿。提供Pareto最佳解决方案进行维修设计,开发方法可以理解为基于纯粹体验的设计决策的有价值的补充。 (c)2020 Elsevier Masson SAS。版权所有。

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